EP1838575B1 - Appareil pour le deploiement de masques a oxygene - Google Patents

Appareil pour le deploiement de masques a oxygene Download PDF

Info

Publication number
EP1838575B1
EP1838575B1 EP06733700.6A EP06733700A EP1838575B1 EP 1838575 B1 EP1838575 B1 EP 1838575B1 EP 06733700 A EP06733700 A EP 06733700A EP 1838575 B1 EP1838575 B1 EP 1838575B1
Authority
EP
European Patent Office
Prior art keywords
cartridge
mask assembly
manifold
opening
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Not-in-force
Application number
EP06733700.6A
Other languages
German (de)
English (en)
Other versions
EP1838575A1 (fr
Inventor
Robert L. SCHAEFFER Jr.
Duard Charles Bennett
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Avox Systems Inc
Original Assignee
Avox Systems Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Avox Systems Inc filed Critical Avox Systems Inc
Publication of EP1838575A1 publication Critical patent/EP1838575A1/fr
Application granted granted Critical
Publication of EP1838575B1 publication Critical patent/EP1838575B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B25/00—Devices for storing or holding or carrying respiratory or breathing apparatus
    • A62B25/005—Devices for storing or holding or carrying respiratory or breathing apparatus for high altitude
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B7/00—Respiratory apparatus
    • A62B7/14—Respiratory apparatus for high-altitude aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2231/00—Emergency oxygen systems
    • B64D2231/02—Supply or distribution systems
    • B64D2231/025—Oxygen masks; Mask storages; Features related to mask deployment

Definitions

  • This invention relates to an apparatus for deploying an emergency breathing mask in an aircraft.
  • the apparatus is automatically or manually operable to present the breathing mask to a user upon loss of cabin pressurization.
  • the masks 16 may have to be replaced after a predetermined period of time, the masks may have to be repacked after inspection or they may have to be repacked after a deployment.
  • components which typically include the oxygen tubes 29, reservoir bag 38, elastic strap 34 and lanyards 60, must be carefully folded and coiled as shown in Fig. 1B so that the mask 16 deploys properly and does not become tangled during an emergency situation.
  • the process of repacking masks is time-consuming and costly given the labor rates of aircraft technicians.
  • the present invention meets the above-described need by providing a method and apparatus for presenting oxygen masks that provides a pre-packaged, modular system that does not require manual repacking of oxygen masks by aircraft technicians.
  • the system also provides a force other than gravity for deploying the masks. It is to be understood that the present invention may be used in a ceiling mounted orientation where it would provide a force in addition to gravity for releasing the masks.
  • a cartridge 100 which may be in the shape of a cylinder, contains a single oxygen mask assembly 103.
  • the oxygen mask assembly 103 may include the following major components: a folded reservoir bag 106, an oronasal mask 109, a strap 112, and breathing conduit 115.
  • the cartridge 100 is provided with side walls 118 and an end wall 121.
  • the end wall 121 is provided with an opening 124 for receiving a quick connect fitting that is in fluid communication with the conduit on the mask assembly.
  • the cartridge 100 Opposite from the end wall 121, the cartridge 100 has an opening 127 where the mask 109 exits the cartridge 100 during deployment.
  • the opening 127 may be initially covered or partially covered by a removable substrate 130 which may be provided with a pressure-sensitive adhesive or the like. Alternately, the substrate 130 may be creased, scored, or perforated such that it will split open during deployment of the mask. The substrate 130 covers the opening 127 to hold the mask assembly 103 in position during installation of the cartridge 100 and may also prevent contamination.
  • the cartridge 100 is a pre-packed standalone assembly that is intended to be installed in the field without requiring any handling of individual mask components by aircraft technicians. Accordingly, the cartridge 100 is provided with quick connect oxygen line connections and quick connect mechanical connections such as quarter-turn bayonet (not shown), pin and slot connections ( Fig. 6-9 ), or "push and stab" connections ( Fig. 12 ) that provide for quick installation in the field without the requirement of tools or separate fasteners. However, it is to be understood that the cartridge 100 can also be installed with tools and separate fasteners.
  • the cartridge 100 includes a supplemental mask ejection device such as the spring-biased piston 131 shown in Fig. 2 .
  • the piston 131 is biased by a pair of coil springs 133 disposed in grooves 135 in the back of the piston 131.
  • the spring 133 is released from a retention mechanism and provides a force on the piston 131 in the downward direction with respect to the orientation of Fig. 2 . This force ejects the mask 109 from its cartridge to present it to the user.
  • the mask ejection device may be formed as part of the cartridge, as part of the housing or oxygen manifold (as shown and described herein in connection with Figs. 10-12 ) or as a part of some or all of the above components.
  • the cartridge in order to eliminate the ejection device from the cartridge, the cartridge may be provided with an end wall that is responsive to force from an ejection device mounted on the manifold.
  • the cartridge may be formed with one or more openings in the top and the one or more openings may be covered by a flexible covering such that the ejection device may act upon the mask 109 to deploy it.
  • a bank of cartridges are shown.
  • cartridge 100 On the left side with respect to the orientation of Fig. 3 , cartridge 100 is shown with the mask removed for clarity.
  • the cartridge 100 includes a quick connect fitting for attaching to a manifold 140.
  • alternate embodiments for the cartridge are shown.
  • a cartridge 150 In the middle position, a cartridge 150 is shown.
  • the cartridge 150 includes a piston 153 sealed with 0-rings 156.
  • the piston 153 is actuated by the pressure of the oxygen and ejects the mask from its cartridge.
  • another alternate gas pressure actuated piston is shown with cup seals 159 to form the pressure chamber above the piston.
  • a pair of cartridges 100 and 150 are shown in relation to the door 160 leading to the inside of the aircraft cabin.
  • the door 160 may be opened by a solenoid-operated actuator 163.
  • the door 160 could be held by a mechanically operated latch capable of being released by the force of the ejection of the mask 109.
  • the mask 109 is ejected from its cartridge by the force of the piston which may be spring-biased or pressure actuated as described above. If the flow of oxygen is initiated when the masks are presented, then the masks may be ejected by pneumatic pressure as described above.
  • mask 109 is ejected from cartridge 180 by a bellows chamber 183.
  • the bellows chamber 183 fills with oxygen causing it to expand and push the mask 109 downward with respect to the orientation of Fig. 5 .
  • Cartridge 200 includes side walls 203 and an end wall 206. Extending from end wall 206 are a pair of studs 209 that can be used for attaching the cartridge 200 to a support structure.
  • the studs have a body portion 212 and an enlarged head 215 for engaging with a slot having an enlarged opening leading to a slot. By inserting the head 215 into the enlarged opening and rotating the cartridge 200, the body portion 212 can be received and retained by the slot as will be evident to those of ordinary skill in the art.
  • an opening 207 surrounded by an adapter 218.
  • the adapter 218 is provided with an O-ring 221 capable of engaging with the oxygen manifold to provide for fluid communication between the oxygen manifold and the oxygen conduit 224 in the cartridge 200.
  • Other connecting means such as quick connects and the like could also be used and the cartridge 200 could therefore be supported from these other structures disposed around the central opening.
  • the adapter 218 leads to a bladder 227 the outlet of which is in fluid communication with the conduit 224.
  • the conduit 224 is coiled above the remaining components such as the reservoir bag, straps, and oronasal mask.
  • a cover 230 is attached to the cartridge 200 at the end opposite from the end wall 206. In operation, the flow of oxygen from the manifold into the bladder 227 causes the bladder 227 to expand and force the mask assembly to push the cover 230 off of the cartridge and causes the mask assembly to exit the cartridge 200.
  • a diaphragm 250 is formed from a flexible sheet of material.
  • the diaphragm 250 may be attached on opposite sides of the cartridge 253 at midwall between the top 256 and bottom 259 of the cartridge.
  • the cartridge 253 has a central opening 268 which is surrounded by a gasket 271 when the cartridge 253 is in position.
  • the central opening 268 is in fluid communication with gas passageway 274 in the manifold 265.
  • a mask assembly 277 (including straps, etc. as described above in connection with Fig. 2 ) is provided for delivering the breathing gas to the user.
  • a hose assembly 280 connects the mask assembly 277 to a fitting 283 on the diaphragm 250.
  • the mask assembly 277 and hose assembly 280 are folded and stowed in the cartridge 253 prior to use (as shown in Fig. 6A ).
  • the flow of breathing gas in the direction of arrow 284 from the manifold 265 causes the diaphragm 250 to move downward with respect to the orientation of Fig. 6B .
  • the force of the diaphragm 250 against the mask assembly 277 causes it to deploy.
  • the force of the diaphragm 250 against the mask assembly 277 provides for deployment of the mask assembly 277 regardless of the location of the cartridge 253 which may include overhead in the ceiling of the aircraft, in the sidewalls of the aircraft, or in the seat assembly.
  • Cartridge 300 has side walls 303 and an end wall 309.
  • the end wall 309 may be provided with studs 312 for engaging with support structure on oxygen manifold 308 ( Figs. 8-9 ) as described above in connection with studs 209.
  • a central opening 310 is surrounded by an adapter 315 having an 0-ring 318 disposed thereon.
  • the adapter 315 may be inserted into the oxygen manifold 308 such that a seal is formed by the 0-ring 318.
  • a spring 321 is seated in a retaining member 323.
  • the retaining member 323 may be provided with a major portion having an H-shape in cross-section.
  • the top section 324 holds the spring 321 and prevents it from making contact with the coiled breathing conduit 327.
  • a tube 330 extends between the adapter 315 and the breathing conduit 327 and is disposed through an opening in the center of the retaining member 323.
  • the bottom of the retaining member 323 is hollow and provides additional support for the coiled breathing conduit 327.
  • the top of the retaining member 323 is provided with a flange 333 that extends outwardly.
  • the spring 321 is compressed between the end wall 309 of the cartridge 300 and the dividing wall 336 in the retaining member 323.
  • the spring 321 is biased against the retaining member 323 in the downward direction with respect to the orientation of Fig. 7 .
  • a latch 350 connected to retaining member 323 holds the spring 321 in the compressed state as shown in Fig. 7 .
  • the latch 350 is engaged with a surface on the oxygen manifold 308.
  • a solenoid actuated piston 360 ( Figs. 8-9 ) may be provided to disengage the latch for deployment of the masks. The piston on the solenoid disengages the latch such that the spring is allowed to expand and push into the mask assembly which in turn pushes against the cover 365 to open the end of the cartridge 300. After the cover 365 is released, the mask assembly exits from the cartridge 300.
  • an alternate embodiment of the invention provides for mounting the springs external to the cartridge.
  • manifold 400 supports a pair of latches having a catch member 403, a shaft 406, a head 409 and a pair of springs 412.
  • the springs 412 are pre-loaded in compression between the head 409 and the bottom surface 415 of the manifold 400.
  • a cartridge 420 has a pair of openings 423 in the top wall for receiving the springs 412 and their supporting structure.
  • the cartridge 420 may be provided with studs 413 for mounting the cartridge 420 on the manifold 400.
  • the cartridge 420 also includes a central opening 426 surrounded by an adapter 429. The central opening is in fluid communication with a breathing conduit 432 connected to an oronasal mask assembly. Accordingly, oxygen from the manifold 400 can flow into the breathing conduit 432 when the cartridge 420 is attached to the manifold 400.
  • a spacer member 430 is disposed between the springs 412 and the mask assembly.
  • a solenoid actuated piston assembly 450 is mounted on the manifold 400 and is disposed such that the pistons disengage the catch members 403 from the oxygen manifold 400. Once the catch members 403 are free, the springs 412 push against the spacer member 430 which pushes the mask assembly against the cover 480 and out of the cartridge 420.
  • the present invention may be used with all types of aircraft supplemental oxygen delivery systems.
  • delivery systems There are two primary types of delivery systems: systems whose deployment is initiated by the turning on of a central oxygen supply and systems whose deployment is initiated by an electrical signal.
  • the pneumatic pressure can be used to push the mask out of its container as described above. Because the containers are normally stored in a housing that typically includes a cover, the pneumatic pressure of the oxygen can be used to unlatch the cover or the cover could be unlatched by the masks pressing against the inside of the cover as they are ejected from their containers.
  • a valve may be inserted in the oxygen supply to prevent a sustained flow of oxygen out through a mask which is not being used. In Fig. 6C , such an arrangement is shown where the valve 285 is inserted at the point where the hose assembly 280 attaches to a fitting 283 on diaphragm 250.
  • the valve 285 may be a simple on/off toggle valve or a clip closing off hose assembly 280.
  • This valve may be attached to a lanyard 288 and when mask assembly 277 is pulled to a user's face, the lanyard 288 will actuate the valve 285 or release the clip allowing oxygen to flow.
  • the valve could also be electronic such that it would be activated by the user's drawing in a breath after donning the mask and creating a slight negative pressure in the mask and tubing, which would be sensed by the electronic switch allowing the oxygen to flow.
  • Fig. 6D illustrates a switch that may be mounted on the manifold or the cartridge. Oxygen flows into a bellows or bladder ejecting the mask as described previously but cannot flow into the tubing of the mask until the electronic valve 289 senses the presence of a user and allows the oxygen to flow to the mask assembly 277.
  • Fig. 6E is a variation of the electronic switch located in the oxygen supply.
  • the electronic switch 296 allows oxygen to flow into the bellows or bladder through central opening 268, ejecting the mask assembly 277 as described previously.
  • the switch 296 is programmed to allow the flow of oxygen to occur for only the length of time needed to eject the mask, after which the oxygen supply is cut off by the electronic switch 296.
  • the electronic switch 296 does not reopen, allowing the flow to continue, until it senses by means of sensor tube 294 that the user is taking a breath.
  • the oxygen source is often a chemical oxygen generator or a sealed oxygen cylinder serving only the group of masks contained in one or more housings.
  • the oxygen supply may be initiated by the users reaching for the oxygen masks and pulling them toward their faces. Accordingly, the ejection of the masks is not associated with the flow of oxygen as the masks have to be ejected prior to actuation of the source of oxygen gas.

Claims (29)

  1. Cartouche (150, 180, 200, 253) destinée à être utilisée avec un collecteur (140, 265), le collecteur (140, 265) ayant une voie de passage en communication de fluide avec une source de gaz respirable, cartouche comprenant :
    - une paroi d'extrémité (206);
    - au moins une paroi latérale (203) s'étendant depuis la paroi d'extrémité (206) et se terminant à une extrémité distale adjacente à une ouverture;
    - un élément flexible (159, 183, 250) définissant une chambre à l'intérieur de la cartouche (150, 180, 200, 253), dans laquelle la chambre est en communication de fluide avec la voie de passage lorsque la cartouche (150, 180, 200, 253) est couplée au collecteur (140, 265), et dans laquelle l'élément flexible (159, 183, 250) a une sortie;
    - un assemblage de masque (109, 277) disposé à l'intérieur de la cartouche (150, 180, 200, 253), l'assemblage de masque (109, 277) ayant un tuyau (280) couplé à la sortie de l'élément flexible (159, 183, 250) de telle manière que la pression contre l'élément flexible (159, 183, 250) causée par l'écoulement du gaz respirable dans la chambre provoque l'éjection de l'assemblage de masque (109, 277) depuis la cartouche (150, 180, 200, 253) à travers l'ouverture à l'extrémité distale de la au moins une paroi latérale.
  2. Cartouche (150, 180, 200, 253) selon la revendication 1, comprenant en outre une bride (218) apte à coopérer avec un élément de verrouillage sur le collecteur (140, 265).
  3. Cartouche (253) selon la revendication 1, dans laquelle l'élément flexible comprend un diaphragme (250).
  4. Cartouche (180) selon la revendication 1, dans laquelle l'élément flexible comprend un soufflet (183).
  5. Cartouche (253) selon la revendication 3, dans laquelle le diaphragme (250) est fixé à un point médian de la au moins une paroi latérale.
  6. Cartouche (253) selon la revendication 3, dans laquelle le diaphragme (250) est fixé à la paroi d'extrémité.
  7. Cartouche (200) selon la revendication 1, dans laquelle la paroi d'extrémité (206) comporte une ouverture (207) définie dans celle-ci, l'ouverture (207) étant en alignement avec la voie de passage lorsque la cartouche (200) est couplée au collecteur (140, 265).
  8. Cartouche (253) selon la revendication 1, comprenant en outre une soupape (285) disposée en relation fonctionnelle avec l'assemblage de masque (277) de telle sorte que la soupape (285) est ouverte pour permettre l'écoulement du gaz respirable à l'assemblage de masque (277) lorsqu'un utilisateur applique une force sur l'assemblage de masque (277).
  9. Cartouche (253) selon la revendication 8, dans laquelle la soupape (285) est actionnée par un cordon (288) fixé à l'assemblage de masque (277).
  10. Cartouche (253) selon la revendication 1, comprenant en outre une soupape réagissant à un utilisateur respirant à travers l'assemblage de masque, la soupape contrôlant le flux du gaz respirable vers l'assemblage de masque.
  11. Cartouche (100, 300, 420) destinée à être utilisée avec un collecteur (308, 400), le collecteur (308, 400) ayant une voie de passage en communication de fluide avec une source de gaz respirable, la cartouche (100, 300, 420) comprenant :
    - une paroi d'extrémité (121, 309) ayant une ouverture (124, 310, 426) définie dans celle-ci, l'ouverture (124, 310, 426) étant en alignement avec la voie de passage lorsque la cartouche (100, 300, 420) est couplée au collecteur (308, 400);
    - au moins une paroi latérale (118, 303) s'étendant depuis la paroi d'extrémité (121, 309) et se terminant à une extrémité distale adjacente à une ouverture (127);
    - un assemblage de masque (109) disposé à l'intérieur de la cartouche (100, 300, 420), l'assemblage de masque (109) ayant un tuyau disposé en communication de fluide avec l'ouverture (124, 310, 426) dans la paroi d'extrémité (121, 309) et,
    - un élément de sollicitation (133, 321, 412) disposé sur une des cartouches (100, 300, 420) et le collecteur (308, 400), l'élément de sollicitation (133, 321, 412) étant disposé dans une configuration normalement fermée adjacent à l'assemblage de masque (109) de telle sorte que l'élément de sollicitation (133, 321, 412) peut être libéré de telle manière qu'il vienne en prise avec l'assemblage de masque (109) pour éjecter l'assemblage de masque (109) à travers l'ouverture (127) à l'extrémité distale de la au moins une paroi latérale (118, 303).
  12. Cartouche (100) selon la revendication 11, comprenant en outre un piston (131) disposé entre l'assemblage de masque (109) et l'élément de sollicitation (133).
  13. Cartouche (300) selon la revendication 11, dans laquelle l'élément de sollicitation (321) est maintenu en position fermée par un verrou (350).
  14. Cartouche (300) selon la revendication 13, dans laquelle le verrou (350) vient en prise avec un cliquet sur le collecteur.
  15. Cartouche (100, 300, 420) selon la revendication 11, dans laquelle un couvercle maintient l'élément de sollicitation (133, 321, 412) en position fermée.
  16. Cartouche (100, 300, 420) selon la revendication 15, dans laquelle le couvercle est ouvert par un verrou actionné par électro-aimant (350, 450) de telle sorte que l'ouverture du couvercle libère l'élément de sollicitation (133, 321, 412) qui à son tour éjecte le masque (109) à travers l'ouverture (127) à l'extrémité distale de la au moins une paroi latérale (118, 303).
  17. Cartouche (300) selon la revendication 11, comprenant en outre un élément de retenue (323) comportant un compartiment destiné à recevoir l'élément de sollicitation (321), l'élément de retenue (323) comportant un verrou (350) qui y est fixé.
  18. Cartouche (300) selon la revendication 17, dans laquelle le verrou (350) sur l'élément de retenue (323) coopère avec un cliquet disposé sur le collecteur.
  19. Cartouche (100, 300, 420) selon la revendication 16, dans laquelle le relâchement du verrou (350, 450) fait que l'élément de sollicitation (133, 321, 412) éjecte un élément de retenue à travers l'ouverture (127) à l'extrémité distale de la au moins une paroi latérale (118, 303).
  20. Cartouche (300) selon la revendication 17, dans laquelle le tuyau s'enroule autour d'une surface extérieure de l'élément de retenue (323).
  21. Cartouche (420) selon la revendication 11, dans laquelle l'élément de sollicitation (412) est relié au collecteur (400) et comprimé contre une surface du collecteur (400) dans la position fermée.
  22. Cartouche (100, 300, 420) selon la revendication 16, dans laquelle l'élément de sollicitation (133, 321, 412) est disposé à l'intérieur de la cartouche (100, 300, 420).
  23. Cartouche (100, 300, 420) selon la revendication 11, comprenant en outre une soupape disposée en relation fonctionnelle avec l'assemblage de masque (109) de telle manière que la soupape est ouverte pour permettre le flux du gaz respiratoire vers l'assemblage de masque (109) lorsqu'un utilisateur applique une force sur l'assemblage de masque (109).
  24. Cartouche (100, 300, 420) selon la revendication 23, dans laquelle la soupape est activée par un cordon attaché à l'assemblage de masque (109).
  25. Cartouche (100, 300, 420) selon la revendication 11, comprenant en outre une soupape réagissant à un utilisateur respirant à travers l'assemblage de masque (109), la soupape contrôlant le débit du gaz respirable vers l'assemblage de masque (109).
  26. Cartouche (100) destinée à être utilisée dans un collecteur (140), le collecteur (14) ayant une voie de passage en communication de fluide avec une source de gaz respirable, la cartouche (100) comprenant :
    - une paroi d'extrémité (121) ayant une ouverture (124) définie dans celle-ci, l'ouverture (124) étant alignée avec le passage lorsque la cartouche (100) est couplée avec le collecteur;
    - au moins un paroi latérale (118) s'étendant depuis la paroi d'extrémité (121) et se terminant à une extrémité distale adjacente à une ouverture (127);
    - un assemblage de masque (109) disposé dans la cartouche (100), l'assemblage de masque (109) ayant un tuyau disposé en communication de fluide avec l'ouverture (124) dans la paroi d'extrémité (121);
    - un piston (153) agencé entre l'assemblage de masque (109) et la paroi d'extrémité (121) de telle manière que le flux du gaz respirable vers la cartouche (100) provoque le coulissement du piston (153) dans l'assemblage de masque (109) provoquant l'éjection de l'assemblage de masque (109) par l'assemblage de masque (109) à travers l'ouverture (127) à l'extrémité distale de la au moins une paroi latérale (118).
  27. Cartouche (100) selon la revendication 26, comprenant en outre une soupape disposée en relation fonctionnelle avec l'assemblage de masque (109) de telle sorte que la soupape est ouverte pour permettre l'écoulement du gaz respirable vers l'assemblage de masque (109) lorsqu'un utilisateur applique une force sur l'assemblage de masque (109).
  28. Cartouche (100) selon la revendication 27, dans laquelle la soupape est activée par un cordon fixé à l'assemblage de masque (109).
  29. Cartouche (100) selon la revendication 26, comprenant en outre une soupape réagissant à un utilisateur respirant à travers l'assemblage de masque (109), la soupape contrôlant le flux du gaz respirable vers l'assemblage de masque (109).
EP06733700.6A 2005-01-13 2006-01-13 Appareil pour le deploiement de masques a oxygene Not-in-force EP1838575B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US64344905P 2005-01-13 2005-01-13
PCT/US2006/001320 WO2006088581A1 (fr) 2005-01-13 2006-01-13 Appareil pour le deploiement de masques a oxygene

Publications (2)

Publication Number Publication Date
EP1838575A1 EP1838575A1 (fr) 2007-10-03
EP1838575B1 true EP1838575B1 (fr) 2013-04-24

Family

ID=36570276

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06733700.6A Not-in-force EP1838575B1 (fr) 2005-01-13 2006-01-13 Appareil pour le deploiement de masques a oxygene

Country Status (8)

Country Link
US (3) US8443802B2 (fr)
EP (1) EP1838575B1 (fr)
JP (1) JP4834000B2 (fr)
CN (1) CN100480136C (fr)
BR (1) BRPI0606694B8 (fr)
CA (1) CA2594877C (fr)
RU (1) RU2007130693A (fr)
WO (1) WO2006088581A1 (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4834000B2 (ja) * 2005-01-13 2011-12-07 エイヴォックス システムズ インコーポレイテッド 酸素マスクを展開するための装置
US8973579B2 (en) * 2005-01-13 2015-03-10 Avox Systems Inc. Self-contained modular deployment system
DE102005044719B4 (de) 2005-09-19 2014-10-30 B/E Aerospace Systems Gmbh Verfahren zum Bestücken einer Passagierversorgungseinheit mit Passagiersauerstoffmasken
DE102006024052B4 (de) * 2006-05-23 2014-09-25 B/E Aerospace Systems Gmbh Flugzeugsauerstoffversorgungseinheit
FR2915788B1 (fr) * 2007-05-04 2012-05-25 Airbus France Dispositif de connexion multi-systemes a bord d'un aeronef
US8393326B2 (en) 2008-01-04 2013-03-12 Intertechnique Device for oxygen supply of a user in an aircraft
DE102010005278A1 (de) * 2010-01-21 2011-07-28 Airbus Operations GmbH, 21129 Sauerstoff-Modul
RU2565387C2 (ru) * 2010-08-26 2015-10-20 Конинклейке Филипс Электроникс Н.В. Система хранения устройства интерфейса пациента
EP2446930B1 (fr) * 2010-10-26 2016-07-13 Zodiac Aerotechnics Dispositif respiratoire à oxygène avec tampon flexible intégré
US9126063B2 (en) * 2010-10-26 2015-09-08 Zodiac Aerotechnics Oxygen breathing device with integrated flexible buffer
US9102417B1 (en) * 2010-12-10 2015-08-11 The Boeing Company Health monitoring system for a vehicle
US8573216B2 (en) * 2011-01-22 2013-11-05 Avox Systems Inc. Vertical drop out box method and apparatus
US8882033B2 (en) * 2011-02-10 2014-11-11 Zodiac Aerotechnics Passenger cabin emergency oxygen device
EP2550994B1 (fr) * 2011-07-25 2014-07-02 Intertechnique Soupape de régulation pour système de survie
US20140000589A1 (en) * 2012-06-28 2014-01-02 Marco Hollm Emergency oxygen device with improved activation lanyard arrangement
WO2014089188A1 (fr) 2012-12-04 2014-06-12 Ino Therapeutics Llc Canule pour réduire au minimum la dilution de dosage pendant l'administration de monoxyde d'azote
US9795756B2 (en) 2012-12-04 2017-10-24 Mallinckrodt Hospital Products IP Limited Cannula for minimizing dilution of dosing during nitric oxide delivery
DE102013220478B4 (de) * 2013-10-10 2022-05-25 B/E Aerospace Systems Gmbh Behältnis mit Abdeckung
CN103830821A (zh) * 2013-12-18 2014-06-04 柳州市华航电器有限公司 一种制氧机的防护外壳
DE102015201124B4 (de) 2015-01-23 2016-08-11 B/E Aerospace Systems Gmbh Sauerstoffmaske
EP3552649B1 (fr) 2015-04-02 2023-08-23 Hill-Rom Services PTE. LTD. Commande de pression de dispositif respiratoire
US10239617B2 (en) * 2015-09-11 2019-03-26 The Boeing Company Oxygen box for a limited maintenance access area above a ceiling panel of an aircraft cabin
DE102017222199A1 (de) * 2017-12-07 2019-06-13 B/E Aerospace Systems Gmbh Sauerstoffversorgungseinrichtung
WO2019161069A1 (fr) * 2018-02-14 2019-08-22 Pacific Precision Products Mfg. Ensemble conteneur de masque d'oxygène d'aéronef
CA3040714A1 (fr) * 2018-04-18 2019-10-18 Zodiac Aerotechnics Un systeme d'oxygene d'urgence destine a un aeronef equipe d'un dispositif de commutation et une methode d'exploitation d'un systeme d'oxygene d'urgence
US11470947B2 (en) 2019-12-20 2022-10-18 Nancy Linday Convertible bag
CN111743259A (zh) * 2020-07-02 2020-10-09 国网北京市电力公司 一种基于气体检测的智能保护装置及方法
CN117048833B (zh) * 2023-07-27 2024-04-19 廊坊翔鲲航空设备有限公司 一种客舱释压供氧装置及控制方法

Family Cites Families (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1699937A (en) * 1927-06-18 1929-01-22 Mine Safety Appliances Co Case for gas masks and canisters
US2931355A (en) * 1957-06-24 1960-04-05 Scott Aviation Corp System for automatically presenting a breathing mask to a person in an emergency
US3277890A (en) * 1963-03-26 1966-10-11 Drager Otto H Closed cycle respirator
GB1097337A (en) * 1964-01-24 1968-01-03 British Aircraft Corp Ltd Improvements relating to oxygen masks for aircraft
US3503394A (en) * 1968-07-22 1970-03-31 Sierra Eng Co Modulized passenger mask assembly
US3615250A (en) * 1969-03-26 1971-10-26 Lockheed Aircraft Corp Supplemental oxygen supply system
US3647165A (en) * 1970-04-27 1972-03-07 Lockheed Aircraft Corp Aircraft compartment and magnetic connecting assembly
US3981302A (en) * 1975-02-26 1976-09-21 Robertshaw Controls Company Emergency breathing means
US4098271A (en) * 1975-09-29 1978-07-04 Mcdonnell Douglas Corporation Oxygen supply system and flow indicator
US4023874A (en) * 1976-02-23 1977-05-17 Mcdonnell Douglas Corporation Oxygen mask stowage
US4154237A (en) * 1977-12-27 1979-05-15 Boeing Commercial Airplane Company Passenger emergency oxygen mask drop zone extender
US4271833A (en) * 1979-06-25 1981-06-09 E. D. Bullard Company Ventilating system for protective clothing
US4481945A (en) 1983-02-10 1984-11-13 Lockheed Corporation Deployment system for emergency oxygen mask
US4710756A (en) * 1985-01-07 1987-12-01 Thornburg Dennis D Combination smoke detector and device for containing air
US4609166A (en) * 1985-02-08 1986-09-02 Ptc Aerospace Inc. Emergency oxygen system for aircraft
FR2586007B1 (fr) * 1985-08-08 1987-12-24 Sfim Dispositif entrebailleur pour porte de boite renfermant un equipement de securite tel que masques a oxygene
DE3610492A1 (de) * 1986-03-27 1987-10-01 Draegerwerk Ag Atemschutzgeraet
DE3613814A1 (de) * 1986-04-24 1987-10-29 Draegerwerk Ag Notversorgungseinheit mit einem atmungsgeraet
DE3719427A1 (de) * 1987-06-11 1988-12-22 Draegerwerk Ag Sauerstoffversorgungseinheit mit einem sauerstoffgenerator zum einbau in fluggeraete
US4909247A (en) * 1988-05-06 1990-03-20 Figgie International, Inc. Aircraft emergency breathing assembly
WO1990002582A1 (fr) 1988-09-14 1990-03-22 Puritan-Bennett Corporation Masque a oxygene pour personnel d'equipage et unite de rangement de tuyau souple
FR2653091A1 (fr) * 1989-10-18 1991-04-19 Graviner Ltd Kidde Dispositif d'alimentation en oxygene.
US5301665A (en) * 1991-05-05 1994-04-12 Dragerwerk Aktiengesellschaft Respirator for emergency oxygen supply for passengers in aircraft
US5154374A (en) * 1991-08-23 1992-10-13 Burns Aerospace Corporation Aircraft passenger seat assembly including an emergency oxygen system
DE4140265C2 (de) * 1991-12-06 1994-11-10 Draegerwerk Ag Behälter für eine Sauerstoffversorgungseinheit
US5408995A (en) * 1993-04-16 1995-04-25 Figgie International Inc. Continuous flow passenger oxygen dispensing unit
US5664566A (en) * 1994-09-30 1997-09-09 Puritan-Bennett Corporation Quick-donning full face oxygen mask with inflatable harness and soft foldable lens
US5803062A (en) * 1996-05-14 1998-09-08 Nellcor Puritan Bennett Inc. Compression molded integrated personal service and oxygen modules for use in transport aircraft with improved mask repacking and test access
US5816244A (en) * 1996-05-14 1998-10-06 Nellcor Puritan Bennett Incorporated Modular structural system for personal service and oxygen dispensing system modules for use in transport aircraft with improved latch and testing capability
DE69732438T2 (de) 1996-06-18 2005-07-07 Itw Ltd., Swansea Verriegelungsvorrichtung
FR2752383B1 (fr) * 1996-08-16 1998-11-06 Intertechnique Sa Equipement de protection respiratoire a indication de mode de fonctionnement
US5954052A (en) * 1997-05-21 1999-09-21 Nellcor Puritan-Bennett Safety stowage apparatus for crew oxygen masks
US6089230A (en) * 1998-11-03 2000-07-18 Be Aerospace Intellectual Property, Inc. Aircraft passenger oxygen delivery unit having shiftable oxygen generating candle
US6336667B1 (en) * 1999-06-11 2002-01-08 B/E Aerospace Intellectual Property Inc. Latch mechanism
US6318364B1 (en) * 1999-07-05 2001-11-20 Be Intellectual Property, Inc. Modular drop out container for aircraft oxygen masks
FR2813061B1 (fr) * 2000-08-17 2002-11-15 Intertechnique Sa Boite a masques respiratoires de secours
FR2813062B1 (fr) 2000-08-17 2002-11-15 Intertechnique Sa Boite a masques respiratoires pour installation de secours
US6526967B2 (en) * 2001-06-11 2003-03-04 Be Intellectual Property, Inc. Crew oxygen mask stowage assembly including selective depressurization valve
US6523539B2 (en) * 2001-07-02 2003-02-25 Be Intellectual Property Inc. Self-elongating oxygen hose for stowable aviation crew oxygen mask
FR2827178B1 (fr) * 2001-07-11 2003-12-05 Intertechnique Sa Appareil respiratoire et installation de protection contre l'hypoxie en comportant application
CN1310801C (zh) * 2002-01-07 2007-04-18 斯考脱航空股份有限公司 阀总管组件
US6755194B2 (en) * 2002-04-09 2004-06-29 Intertechnique, S.A. Stowage systems, particularly for oxygen masks
GB0301934D0 (en) * 2003-01-28 2003-02-26 Sundar Satish Delivery apparatus and location method
US7331979B2 (en) * 2003-06-04 2008-02-19 Access Closure, Inc. Apparatus and methods for sealing a vascular puncture
DE10337694A1 (de) * 2003-08-16 2005-03-10 Airbus Gmbh Verfahren zur Präsentation von Sauerstoffmasken in der Kabine eines Flugzeuges
DE102004009346B4 (de) * 2004-02-26 2008-07-24 Airbus Deutschland Gmbh Klappenanordnung für O2 Maskencontainer
DE102004026649A1 (de) * 2004-06-01 2006-01-05 DRäGER AEROSPACE GMBH Sauerstoffnotversorgungseinrichtung
JP4834000B2 (ja) * 2005-01-13 2011-12-07 エイヴォックス システムズ インコーポレイテッド 酸素マスクを展開するための装置

Also Published As

Publication number Publication date
US8443802B2 (en) 2013-05-21
JP2008526447A (ja) 2008-07-24
CN101107165A (zh) 2008-01-16
BRPI0606694B8 (pt) 2019-10-15
US8356595B2 (en) 2013-01-22
CA2594877C (fr) 2014-06-17
BRPI0606694B1 (pt) 2019-07-09
WO2006088581A1 (fr) 2006-08-24
US20090151727A1 (en) 2009-06-18
JP4834000B2 (ja) 2011-12-07
BRPI0606694A2 (pt) 2010-01-12
EP1838575A1 (fr) 2007-10-03
US20060169283A1 (en) 2006-08-03
CN100480136C (zh) 2009-04-22
CA2594877A1 (fr) 2006-08-24
RU2007130693A (ru) 2009-02-20
US20070246048A1 (en) 2007-10-25

Similar Documents

Publication Publication Date Title
EP1838575B1 (fr) Appareil pour le deploiement de masques a oxygene
US8973579B2 (en) Self-contained modular deployment system
US4909247A (en) Aircraft emergency breathing assembly
US4559939A (en) Compatible smoke and oxygen masks for use on aircraft
JP2005500098A (ja) 選択的な減圧バルブを含む乗務員酸素マスク積込アセンブリ
EP1465805B1 (fr) Ensemble collecteur de soupape
EP2665525B1 (fr) Procédé et appareil de présentation automatique verticale de boîtier
JP2016506252A (ja) 航空機洗面所酸素源
US10974832B2 (en) System for the emergency oxygen supply of passengers in an aircraft
US10823300B2 (en) Aspirator pressure relief valve with relief control unit
EP1474329B1 (fr) Dispositif de reglage de clapet pour distributeur de masque a oxygene
CN114375217B (zh) 用于向乘客递送呼吸气体的系统
US11009140B1 (en) Self-closing valve

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20070813

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

RIN1 Information on inventor provided before grant (corrected)

Inventor name: HOLLEY, KRISTINE

Inventor name: KEISER, NISHLA

Inventor name: CHANDRASEKARAN, AARTHI

Inventor name: KIZILTEPE BILGICER, TANYEL

Inventor name: SENGUPTA, SHILADITYA

Inventor name: SANFILIPPO, STEVEN, M.

Inventor name: BERRY, DAVID A.

Inventor name: SCHAEFFER, ROBERT, L., JR.

Inventor name: BENNETT, DUARD, CHARLES

Inventor name: EAVERONE, DAVID

RIN1 Information on inventor provided before grant (corrected)

Inventor name: SENGUPTA, SHILADITYA

Inventor name: BERRY, DAVID A.

Inventor name: EAVERONE, DAVID

Inventor name: KEISER, NISHLA

Inventor name: HOLLEY, KRISTINE

Inventor name: CHANDRASEKARAN, AARTHI

Inventor name: KIZILTEPE BILGICER, TANYEL

Inventor name: SCHAEFFER, ROBERT, L., JR.

Inventor name: BENNETT, DUARD, CHARLES

RIN1 Information on inventor provided before grant (corrected)

Inventor name: BENNETT, DUARD, CHARLES

Inventor name: SCHAEFFER, ROBERT, L., JR.

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20120315

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602006035886

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: B64D0011000000

Ipc: A62B0007140000

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

RIC1 Information provided on ipc code assigned before grant

Ipc: A62B 7/14 20060101AFI20121004BHEP

Ipc: B64D 11/00 20060101ALI20121004BHEP

Ipc: A62B 25/00 20060101ALI20121004BHEP

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

RIN1 Information on inventor provided before grant (corrected)

Inventor name: BENNETT, DUARD CHARLES

Inventor name: SCHAEFFER, ROBERT, L. JR.

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 608231

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130515

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602006035886

Country of ref document: DE

Effective date: 20130620

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 608231

Country of ref document: AT

Kind code of ref document: T

Effective date: 20130424

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20130424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130826

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130725

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130804

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130824

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130724

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20140127

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602006035886

Country of ref document: DE

Effective date: 20140127

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140113

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140131

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140131

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140113

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20130424

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20060113

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20201217

Year of fee payment: 16

Ref country code: GB

Payment date: 20201218

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20210104

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20201217

Year of fee payment: 16

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602006035886

Country of ref document: DE

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20220113

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220113

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220802

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20220113